Aero Classes > Individual calculation
Perform CFD calculation for a given cross-section.
Setting | Description |
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Wind direction, Alpha, v-ref | Attack angle (angle of incidence, angle between the local z-axis of the element and the wind direction, positive from +z to the wind direction in direction +y) and velocity |
Suggest | Create default values for selected cross section and wind direction/velocity |
dt, Iter | Time step for integration and number of time steps |
Nr. of panels, Core size | Number of surface panel on CS and size of vortex particles. Control spatial resolution. |
More options... | Enable multithreading and export of time history, impose forced cross section oscillation |
Set param. | Save currently active set of parameters to aero class |
Get param. | Restore previously saved set of parameters |
Group, Name | Group and name of current cross-section. |
Recalc, Pause, Cancel, Continue | Control calculation |
Option: Create movie, Options | Save graphical representation to AVI file. Options allows to give resolution and file name. |
Graphical representation |
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